3D flight track and 6-DOF flight simulation based on Google Earth

2010 ◽  
Vol 29 (12) ◽  
pp. 3385-3387 ◽  
Author(s):  
Yong TANG ◽  
Chang-zhong LIU ◽  
Hong-gang WU
Keyword(s):  
Google Earth ◽  
Flight Simulation ◽  
Simulation Based

Real-time 3D flight track and flight simulation based on Google Earth

2012 ◽  
Vol 6 (19) ◽  
pp. 385-392 ◽  
Author(s):  
TANG Yong ◽  
WU Honggang ◽  
LIU Pengfei ◽  
SI Quan
Keyword(s):  
Real Time ◽  
Google Earth ◽  
Flight Simulation ◽  
Simulation Based

Research on Simulation Modeling of Flight Aircraft Air under the Condition of Turbulent Flow

2014 ◽  
Vol 684 ◽  
pp. 165-168
Author(s):  
Yong Zhou Jiang ◽  
Yong Ji Lu ◽  
Yan Ding ◽  
Xiao Yan Yu
Keyword(s):  
Real Time ◽  
Simulation Modeling ◽  
Flight Simulation ◽  
Flight Simulator ◽  
Aircraft Structure ◽  
Atmospheric Disturbance ◽  
Real Time Simulation ◽  
Time Simulation ◽  
Simulation Based ◽  
Long Time

The flight process often in turbulence. Atmospheric turbulence causes flight bump, long time will cause damage to the aircraft structure fatigue. This paper establishes a model for atmospheric disturbance, flight simulation. Based on the aircraft through all kinds of atmospheric disturbance is studied. The use of embedded database and real-time simulation platform, built a run, in the PC machine can be used for dynamic model for real-time simulation of flight simulator.

Improving the Error Model for POS Applicationto Airborne InSAR

2012 ◽  
Vol 239-240 ◽  
pp. 521-529
Author(s):  
Lin Zhou Ting Chen ◽  
Jian Cheng Fang
Keyword(s):  
Measurement Errors ◽  
Constant Error ◽  
Inertial Sensor ◽  
Error Model ◽  
Flight Simulation ◽  
First Order ◽  
Process Error ◽  
Simulation Based ◽  
Orientation System ◽  
Flight Route

Position and Orientation System (POS) is a technology widely used for motional error compensation of airborne InSAR. The measurement errors of inertial sensor (accelerometers and gyros) are the chief influencing factors to the precision of POS. In order to enhance the accuracy of POS, an improved SINS error model should be used in POS. In this paper, a more precise error model for SINS is developed by augmenting random walks error, first-order Markov process error, scale factor error and installation error. To validate the accuracy of the improved error model, semi physical flight simulation based on the imitation of imaging-flight route of InSAR is made to compare with the traditional SINS error model which only considering the random constant error. The simulation results show that the accuracy of the improved SINS error model is one order higher than the traditional SINS error model.

Simulation-Based Helicopter Mission Effectiveness Evaluation Method

2014 ◽  
Vol 651-653 ◽  
pp. 962-965
Author(s):  
Ji Cai ◽  
Hu Liu ◽  
Hong Tang
Keyword(s):  
Evaluation Method ◽  
Weight Coefficient ◽  
Flight Simulation ◽  
Effectiveness Evaluation ◽  
Simulation Data ◽  
Advantages And Disadvantages ◽  
Helicopter Flight ◽  
Parameter Evaluation ◽  
Simulation Based ◽  
Mission Effectiveness

It is always difficult to obtain a reliable result of helicopter mission effectiveness evaluation (HMEE) by traditional methods. In order to solve the problem, this paper compared and analysed advantages and disadvantages of traditional effectiveness evaluation methods, and presented a simulation-based helicopter mission effectiveness evaluation method. The method is based on the simulation data. The method combines with advantages of multi parameter evaluation method, computer simulation evaluation method and logarithmic evaluation method. By using the reliable helicopter flight simulation data and an objective weight coefficient calculation methods, we can get accurate and reliable helicopter mission effectiveness value. Research proves that this method can be applied in the field of effectiveness evaluation.

Returning to flight: simulation-based training for the US National Aeronautics and Space Administration's Space Shuttle Mission Management Team

2007 ◽  
Vol 11 (2) ◽  
pp. 132-138 ◽  
Author(s):  
Cameron Klein ◽  
Kevin C. Stagl ◽  
Eduardo Salas ◽  
Christopher Parker ◽  
Donald F. Van Eynde
Keyword(s):  
Space Shuttle ◽  
Flight Simulation ◽  
Management Team ◽  
Simulation Based ◽  
The Us ◽  
Mission Management

Wake Vortex Model for Real-Time Flight Simulation Based on Large Eddy Simulation

2007 ◽  
Vol 44 (2) ◽  
pp. 467-475 ◽  
Author(s):  
Graham T. Spence ◽  
Alan Le Moigne ◽  
David J. Allerton ◽  
Ning Qin
Keyword(s):  
Large Eddy Simulation ◽  
Real Time ◽  
Flight Simulation ◽  
Wake Vortex ◽  
Vortex Model ◽  
Eddy Simulation ◽  
Simulation Based ◽  
Large Eddy

scholarly journals The use of modern simulator technologies in air training on the example of the air force university in Deblin

2019 ◽  
pp. 24-31
Author(s):  
Henryk Nowakowski ◽  
Jaroslaw Kozuba
Keyword(s):  
Air Force ◽  
Simulation Training ◽  
Training System ◽  
Flight Simulation ◽  
Flight Training ◽  
Teaching Process ◽  
Flight Simulators ◽  
Simulation Based ◽  
The University

The article presents flight simulation training devices used for the training of students at Dęblin Air Force University from the early 60s until the present time. It includes information concerning the scope of the use of training devices in the teaching process as well as training itself of the university flying personnel. It also presents the development of flight simulation based on changes in the devices facilitating flight training, from training devices to the Integrated Training System. The use of flight simulators for the training of pilots is becoming an increasingly more important element of this training. More and more advanced flight simulators allow the implementation of the majority of flight procedures.

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